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Discrete-time output feedback sliding-mode control design for uncertain systems using linear matrix inequalities

机译:基于线性矩阵不等式的不确定系统离散输出反馈滑模控制设计

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摘要

An output feedback-based sliding-mode control design methodology for discrete-time systems is considered in this article. In previous work, it has been shown that by identifying a minimal set of current and past outputs, an augmented system can be obtained which permits the design of a sliding surface based upon output information only, if the invariant zeros of this augmented system are stable. In this work, a procedure for realising discrete-time controllers via a particular set of extended outputs is presented for non-square systems with uncertainties. This method is applicable when unstable invariant zeros are present in the original system. The conditions for existence of a sliding manifold guaranteeing a stable sliding motion are given. A procedure to obtain a Lyapunov matrix, which simultaneously satisfies both a Riccati inequality and a structural constraint, is used to formulate the corresponding control to solve the reachability problem. A numerical method using linear matrix inequalities is suggested to obtain the Lyapunov matrix. Finally, the design approach given in this article is applied to an aircraft problem and the use of the method as a reconfigurable control strategy in the presence of sensor failure is demonstrated.
机译:本文考虑了用于离散时间系统的基于输出反馈的滑模控制设计方法。在先前的工作中,已经表明,通过识别当前和过去的输出的最小集合,可以得到增强系统,如果该增强系统的不变零是稳定的,则该增强系统仅允许基于输出信息来设计滑动表面。 。在这项工作中,针对具有不确定性的非平方系统,提出了通过一组特定的扩展输出来实现离散时间控制器的过程。当原始系统中存在不稳定不变零时,此方法适用。给出了确保歧管稳定滑动的滑动歧管的存在条件。使用同时满足Riccati不等式和结构约束的Lyapunov矩阵的获取过程来制定相应的控件,以解决可达性问题。建议使用线性矩阵不等式的数值方法来获得李雅普诺夫矩阵。最后,将本文给出的设计方法应用于飞机问题,并演示了该方法在存在传感器故障的情况下作为可重构控制策略的使用。

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